DECOMPRESSION MACHINE (SUDARSHAN CHAKRA)
SU [good], DARHAN [looking;appearance] CHAKRA [wheel]

ABSTRACT

A decompression machine to be called SUDARSHAN CHAKRA is a better efficiency of energy conversion method than prior arts i.e. turbine, internal combustion engine &amp; steam engine. Gas or liquid containing intermolecular forces from anywhere is harnessed &amp; released intra-corporally &amp; sequentially to get discharged tangentially from the blades which absorb the momentum of the propellant by pressure drops &amp;/or velocity rises, in order to produce torque force resulting into rotations of axle, which can drive any other machine for production or transfer of energy. This is an action&amp; reaction turbine. Here the idea is to produce circular motion from natural linear motion of the propellants like wind, gas, steam, water, hydrocarbon Etc.

CROSS REFERENCE TO RELATED APPLICATION

EFS ID—5769743

Provisional application No. 61/228550

BACKGROUND & DISCUSSION OF PRIOR ART

This machine is for use in energy sector where different types ofconversion machines; to convert potential &/or kinetic energy intokinetic energy of a rotating wheel; using well known techniques' ofsteam engine, internal combustion engine & turbine arrangements arealready existing.

Attempts of using compressed air to run different vehicles appearfrequently in news articles. The main hurdle to its market success isthe need of a large size of compressed air tank which is mainly due topoorer efficiency of these conversion machines. These well known priorarts conversion machines namely steam engine, internal combustionengine, turbines & jet engine use compressed steam, gas, water & burnthydro carbon-gas mixtures; to be called propellant; as source ofpotential energy, which is allowed to strike on the outer surface ofturbine blades or piston; to be called receptor; of piston-crank-shaftassembly. These receptors are solid objects & not hollow like SUDARSHANCHAKRA.

I have no information about any published article or any machine inpublic, private or commercial use as well as any invention in progress,which utilizes hollow radial or tangential blades attached upon a hollowmini-axle or mega-axle to absorb momentum from the energy stored in thepropellant flowing through its internal space to generate kinetic energyof a rotating wheel as a circular motion from a linear motion.

The energy production & transfer is so far done by transferringintermolecular forces stored in gas or liquid (propellant) to a wheelenabled to rotate by direct colliding action of the molecules of thepropellant either upon the outer side of the blades of the turbine orupon a reciprocally movable piston-crank assembly inside the cylinder.None of the wheels are enabled to rotate in response to active &reactive forces acting upon the inner side of the blades byintra-corporal flow of intermolecular forces of propellant. Theinvention set forth here has a novel feature. It is an action & reactionturbine with an intra-corporal flow of the propellant. In all of thesemethods molecules propel the blades in direction of their own flow,hence may be said to be unidirectional synchronous motion. Theintermolecular motions strike for a very brief period of time & some ofthe molecules may even fail to strike the blades; hence their energygoes in vain in these prior arts. So their output is considerably smallas compared to input. In the invention set forth it is seen thatrotations of the rotor takes place in the direction opposite to thedirection of the flow of the stream; so this is a sum total of theaction & reaction forces & may be called a counter directionalsynchronous motion.

Here the flow comes from back or front side of the blades & strike uponthe inner side of the bottom wall; to be called receptor; of thesucceeding Tunnel, after taking a U turn to deliver an action of thepropellant from its nozzle like tip to be called inducer. Therefore theinvention set forth tries to address the issue with novelty as well asefficiency.

This is an action & reaction turbine. The machine gradually allows theseforces to get discharged & very large surface area is provided for theaction of flow to exert their forces, so the molecules strike morefrequently to the blades. Hence more impact of the intermolecular forcesare exerted upon the assembly than the prior art therefore moreaction-reaction response can be generated in the form of output. Thepressure & velocity drops can be planned & staged in different Tunnelsas the end application needs. In short the energy extracted from the setforth invention would be larger than the prior arts from any giveninput.

OBJECTS

The object of the invention set forth is to harness & convert maximumamount of intermolecular energy in the from natural linear velocity ofmolecules into circular velocity of gear; of the given gas or liquid(propellant) containing potential energy into a kinetic energy of a gearwhich can rotate the other wheels for numerous uses.

-   -   [1] It is an object of the present invention to produce a torque        force upon a pulley or a gear attached upon the outer surface of        the axle by the reaction of the active force flowing out        [discharging] from the outlets of the blades forcefully by        providing a corrugated inner surface lining of the Case which        very close but clearly away from the outlets. This will also        help to overcome the inertia of the assembly at the beginning of        the rotations.    -   [2] It is an object of the present invention to maximize the sum        total of the action & reaction forces flowing through the        assembly & extract energy with high efficiency, from the energy        of the stream with uniform changes of the ordered directions of        the Tunnels at different places called Nodes on the blades. The        pressure drops & velocity rises take place in the blades which        absorbs majority of the momentum enabling it to rotate in the        desired direction.    -   [3] It is an object of the present invention to provide a        cavernous axle with numerous perforations upon its body for        attaching blades with their inlets opening near the axis; an        open mouth with a flange for attaching the outer diameter of the        mouth bearing; and a closed tail end with a flange for attaching        the inner diameter of tail bearing and places for attaching two        safety valves. A place upon the outer side of the axle is also        provided to attach a pulley or gear.    -   [4] It is an object of the present invention to prevent        significant reduction of pressure in the streams as they go from        axle to the outlets by providing larger inlets than the outlets        of the blades. The parts of Tunnel 1, 2, 3 . . . may be formed        like converging or non converging nozzle to generate pressure        &/or velocity drops whatever is desirable.    -   [5] It is an object of the present invention is extract as much        energy as possible by gradual discharge with minimal pressure &        velocity of the flow from the outlets by keeping converging        nozzle like Tunnels with frequently bending at Nodes having        constricted & enlarged diameters of Tunnels to absorb maximum        momentum from molecules.    -   [6] It is an object of the present invention to keep on        transferring the torque of axle to the machine desired to be        driven by Sudarshan chakra, by providing a pulley or a gear on        the outer surface of the axle kept preferably midway between        mouth & tail.    -   [7] It is an object of the present invention to keep the axle        free to rotate by providing a ball bearing at the junction part        of the mouth of the axle & feeder pipe fixed to inner diameter        of the bearing to be kept stationary as well as fixed to the        frame.    -   [8] It is an object of the present invention to attach        stationary outer diameter of the tail bearing to frame & inner        diameter attached to mobile axles' outer surface by providing a        tail ball bearing so the axle is free to rotate.    -   [9] It is an object of the present invention to prevent blow up        of the assembly due to undesirable excessive rise in the intra        corporal pressure by providing two safety valves preferably near        tail.

SUMMARY OF INVENTION

Intermittently indefinitely & weakly flowing natural forces like wind,tide, water streams & solar energy can be harnessed & gathered in theform of potential energy of compressed air which can be used to driveSUDARSHAN CHAKRA, that will drive any machine for instance electricturbine to generate energy continuously.

BRIEF SUMMARY OF SEVERAL VIEWS OF DRAWING

FIG. 1 Separate Parts

FIG. 2 Elevation View of Assembly

FIG. 3 Isometric View of Assembly

FIG. 4 Cross Section of Assembly

FIG. 5 Cross Section of Assembly

FIG. 6 Cross Section of Ramification

FIG. 7 Elevation View of Ramification

FIG. 8 Top View of Ramification

DETAILED DESCRIPTION OF STRUCTURES OF SUDARSHAN CHAKRA

Assembling stationary parts with junction parts & mobile parts makes afull Sudarshan chakra. Assembling a cavernous mini-axle (2A) withnumerous blades (3), two ball bearings, two safety valves (8) & a pulleyor gear (6) forms the main central mobile part of the assembly. Thenthese mobile parts are fixed with in the grip of stationary parts namelya Feeder pipe (7) at mouth bearing and a cylindrical Case (1) & a stand.

The cavernous elongated hollow pipe of any cross sectional shape havingan open mouth flange which is to be attached to the outer diameter ofmouth bearing; a hollow body with numerous perforations for attachmentsof blades (3) and a closed tail end with flange for attachment of theinner diameter of tail bearing; may be called mini-axle (2A). Thismini-axle (2A) may or may not be supported by mega-axle (2B) if needdemands. Two safety valves (8) preferably near the tail are provided tovent out extra pressure. A pulley or a gear (6) is fixed on the outersurface of the mini-axle (2A) preferably midway between the mouth &tail. The blind end of the cavernous mini-axle (2A) may be enlarged likea pouch to create reserve supply if needed or may be attached to anotherFeeder pipe (7).

The blades (3) are hollow bow shaped structure having any crosssectional & longitudinal sectional shapes like round, oval, elliptical,triangular, square, rectangular or polygonal. This variable part isattached to a hollow mini-axle (2A) or mega-axle (2B) with angularorientation. The larger opening of the blade (3) near mini-axle (2A) iscalled inlet. The smaller opening near the Case (1) is called outlet.The hollow space inside the blade (3) is called tunnel, which issubdivided into Tunnel-0, Tunnel-1 and Tunnel-2 . . . . The blades (3)bend clockwise, anticlockwise spirally up or down as one proceeds frominlet to outlet. There are sudden modifications in the course of tunnelcalled node (3 a) at the junction of Tunnel-0-1-2-3 . . . . The aim ofkeeping nodes (3 a) is to bring about pressure & velocity drops totransfer momentum as well as to carry forward the conserved momentum fornext momentums' transfers.

All the nodes (3 a) upon each blade (3), which are most proximal toaxle& axis may be grouped and named as node-A. The next distal group ofnodes (3 a) upon all the blades (3) may be called Node-B. The nextdistal group of nodes (3 a) upon all the blades (3) may be called Node-Cetc so on & so forth . . . . Similarly the parts of the tunnels (3 b) ofall the blades (3) may be grouped as Tunnel-0 between axis and Node-A,Tunnel-1 between Nodes (3 a)-A & Node-B, Tunnel-2 between Node-B &Node-C, so on & so forth . . . .

The blades (3) of Sudarshan chakra can be regrouped into numerousmodules according to their plane of attachment to the mini-axle (2A) orMega-axle (2B). The group of blades (3) attached to the mini-axle (2A)or mega-axle (2B); in one cross sectional plane may be defined as amodule. These modules may be named as Module-1, Module-2, and Module-3,so on & so forth Each module may contain a variable number of blades(3), but they are identically oriented & balanced upon the mini-axle(2A) or Mega-axle (2B). The member blades (3) of each module spread outuniformly either in the same plane or traverse across neighboring planesto orient spirally up or down. Hence the relationship between axis & anygiven part of a blade (3) is identical with the corresponding part ofany other blade (3).

In other words the blades (3) are designed in such a way that Node-A ofeach blade (3) is oriented at the circumference of an imaginarycylindrical wall around the axis and Tunnel-1 of each blade (3) is astangential as possible to that imaginary cylindrical wall havingimaginary radius joining Node-A to & axis. Similarly Node-B of eachblade (3) is oriented at the circumference of another larger imaginarycylindrical wall around axis; and Tunnel-2 as tangential as possible tothat imaginary cylindrical wall, upon an imaginary line as a radiusjoining Node-B to the axis. Again Node-C of each blade (3) is orientedat one larger circumference of an imaginary cylindrical surface &Tunnel-3 as tangential as possible to that surface upon an imaginaryradius joining Node-C & axis . . . so on & so forth . . . .

The hollow space within the blades (3) called tunnel is furthersubdivided into different parts as follows. The part of tunnel mostproximal to axis from inlet to Node-A may be called Tunnel-0, which canbe in radial to tangential orienting direction of the mini-axle (2A) orthe mega-axle (2B). The next distal group sections of tunnel from Node-Ato Node-B may be called Tunnel-1 which is tangential to imaginary radiusjoining the axis to Node-A. The next distal group of sections of tunnels(3 b) from Node-B to Node-C may be called Tunnel-2 which is tangentialupon an imaginary radius joining Node-B to the axis of the axle.Similarly the next distal group of sections of tunnels (3 b) from Node-Cto Node-D may be called Tunnel-3 which is tangential upon an imaginaryradius joining Node-C to the axis. So on & so forth . . . . Hence allthe sections of tunnel namely Tunnel-0, Tunnel-1, Tunnel-2, Tunnel-3etc., so on & so forth . . . are all outside the mini-axle (2A) andradial to tangential in direction. The tunnels (3 b)′ diameter may beconstricted & enlarged at the nodes (3 a) depending on the need. Theinner shape of the tunnels (3 b) may or may not be made like converging,non-converging or diverging nozzle to effect pressure &/or velocitydrops & absorb the momentum of molecules from propellant. The objectiveof providing numerous Nodes (3 a) like A, B, C . . . so on & so forth &Tunnels 1, 2, 3 . . . so on & so forth, is to absorb as much momentum aspossible within the blades (3), so that the loss of energy at theoutlets (3 c) is minimal.

For practicality of operation one more axle which may be calledMega-axle (2B) can be planned & applied for better stability. This newlayer to be called Mega-axle (2B) is interposed between mini-axle (2A) &the blades (3), so that the mini-axle (2A) & Mega-axle (2B) needs to beattached with each other by a leak proof ring gasket. The blades (3) areattached to Mega-axle (2B) instead of mini-axle (2A). Hence a cavernousmini-axle (2A) opens into Mega-axle (2B) & Mega-axle (2B) opens intoTunnel-0 of the blades (3). The cross section of the blades (3) may bekept circular, oval, elliptical, triangular, square, rectangular orpolygonal, as the end application needs. Practically Tunnel-0 can beattached at any angle from radius to tangent to the Mega-axle (2B)Tunnel-1, 2, 3, 4 - - - may be attached to Mega-axle (2B) by Pillars forbetter stability.

In the given example of drawing no. 2, 3, 4 there are three blades (3)in one module. Each blade (3) has Tunnel 0, 1, 2, 3, Tunnel-0 begins atinlet & ends at Node-A. the most proximal part having wedge shapedhollow body with broad base of the bottom wall called receptor & atapering tip; to be called inducer (3 e); taking U turn inwards oroutwards to open opposite to bottom (receptor) of the succeeding Tunnelcalled Tunnel-1. The planes of the broad base bottom walls (receptors(30) are oriented in such a way that they are parallel to the radialplane of the mini-axle (2A)& mega-axle (2B). Similarly Tunnel-1 is alsoa wedge shaped hollow structure with broad base bottom wall (receptor) &tapering tip (inducer (3 e)) taking U turn to open in front of thebottom wall (receptor) of the succeeding tunnel segment calledTunnel-2.for practical use the sidewalls of Tunnel 0, 1, 2, 3 . . . canbe interlinked & joined to the pillar erected upon axle in radialdirection for the sake of stability. The purpose of such design is toabsorb as much momentum as is possible from the propellant flowingthrough the tunnels (3 b).Parts of all the Tunnels (3 b) exceptTunnel-0; near their broad bottom wall to be called receptor; act assegments of the propelling blade (3) of the turbine. At the tip they actas a nozzle (inducer (3 e)) to shower high velocity stream upon thebottom wall to be called receptor of the succeeding Tunnel Hence unusedmomentum is carried forward for further momentum transfer during thesubsequent course. So the tunnels act as receptor as well as inductortwo in one.

The virtual mean momentum transfer plane can shrink & enlarge accordingto the load & feed quality to provide differential efficiencies as perthe end application needs.

In the given drawing no:4,5 the cross section of the Tunnel is keptrectangular & longitudinal section of the Tunnel is kept triangular withits tip (inductor) taking a U turn before it opens opposite to the broadbottom wall (receptor) of the succeeding Tunnel Thus the entire tunnelof the blade (3) converges as it approaches the Node & diverges as soonas it crosses the Node.

The Case (1) is a realistic cylindrical wall with corrugated innerlining on surface which is just opposite but clearly away from theoutlets (3 c) of all the blades (3). The Case (1) engulfs the assemblylike a sleeve cover with its axis merging with the axis of the mini-axle(2A) Due to closed tail end it is necessary to provide safety valve (8)near the tail end to vent out undesired rise in the intra corporalpressure of the mini-axle (2A) to prevent blow up of the assembly.

The Feeder pipe (7) is attached to the inner diameter of the mouthbearing to feed gas or liquid stream into the mini-axle (2A).

For variation one can keep Tunnel semi flexible as shown in FIGS. 6, 7,and 8 Thus the inner diameter of mouth bearing with Feeder pipe (7) theouter diameter of tail bearing and the Case (1) are stationary partsattached to the frame; whereas there moving parts namely the outerdiameter of mouth bearing, entire cavernous mini-axle (2A), mega-axle(2B), blades (3), safety valve (8), a pulley or gear and the innerdiameter of the tail bearing are free to rotate within the grip ofstationary parts, around imaginary axis joining centers of mouth andtail bearing. The balls inside the mouth & tail bearings facilitatethese movements

OPERATION OF INVENTIONS

When hose from supply tank is connected to the Feeder pipe (7) of theassembly in a leak proof manner & gas or liquid is allowed to flow withforce into the axle, it will rotate along with its attachments with inthe grip of stationary parts & the rotating pulley or gear will transferits torque to the machine desired to be driven by Sudarshan chakra.

The molecules of gas or liquid are in constant motion. When theirstreams are allowed to flow with additional accelerating forces likecompression, heat, velocity or gravity; their motions become extremelypowerful carrying energy of accelerating forces with in their flow.

When stream of gas or liquid flows through the cavernous axle, it splitsup into smaller streams passing through numerous bent blades (3)uniformly in predetermined course to exit from the outlets (3 c). Themolecules experience a lot of friction due to a large surface area&constrictions within the assembly & there are numerous drops of pressure& rises in velocity in different parts. The action of force generatesmomentum which is absorbed by different parts of the blades (3) &collectively produces action-reaction in the form of rotations of theassembly in the direction opposite to that of the stream.

Hence the flow through constrictions to be called inducer (3 e) at thenodes (3 a) from the pool of molecules under the pressure generatesaction & reaction in the opposite directions using Newton's third law ofmotion to provide useful rotations of the axle & gear in the desireddirection.

It is also evident from the performance that synergy of the actionforces reaction forces also exist in the given machine. As per Newton'sfirst law of motion the body at rest or in velocity or remains in statusco unless force is provided.

Here the direction & hence velocity of molecules is changed tangentiallyso force & its reaction are generated. Direct impact of high velocitymolecules in the stream of the flow colliding upon the inner side of thebottom wall to be called receptor; which is directed with radialorientation to the mini-axle (2A) & mega-axle (2B) uses Newton's firstlaw of motion.

According to Newton's third law of motion, the action and reaction of agiven force are equal & opposite. Here action is exerted by the stream &reaction is expressed in the rotation of axle in the opposite direction.The corrugated inner wall of the Case (1) helps to exert final reactivepush to the assembly while the stream exits from the outlet. Theserotations will continue till the flow of the stream is stopped.

The nodes (3 a) act as a strainer allowing the flow with rise invelocity & fall in pressure. Inducer (3 e) acts as a nozzle & receptoracts as a blade (3) segment.

High pressure gas or liquid strained through different parts of theblades (3) leads to momentum transfer from gas or liquid to the blades(3) to generate rotations & torque of the axle for useful work.

In other words the axle will rotate in the direction opposite to that ofthe stream, in order to relieve the pressure inside it by facilitatingrotations to evacuate gas or liquid as fast as possible. Hence theoutput of this machine would be larger than that of the prior arts fromany given input due to many factors integrated in the invention.

The performance or output of SUDARSHAN CHAKRA will be directlyproportional to diameters of inlets (3 d), numbers of nodes (3 a) anddistance between axis to nodes, total inner surface area of blades (3),pressure drops & velocity rises. It will be inversely proportional tothe distance between inducer (3 e) & receptor, diameters of outlets (3c), intra corporal volume of axle & distance between outlets (3 c) toinner wall of the Case (1).

RAMIFICATION

For simplicity of understanding the axle is given names like tail end &mouth end by keeping feeder pipe only at one end of the axle. But if endapplication needs one can keep feeder pipe at both the ends of the axle.

For simplicity of understanding the mouth bearing is kept inside theaxle & tail bearing is kept on the outer side of the axle. But if theend application needs the mouth bearing & tail bearing can be kept inany permutation & combination order of their position upon the axle.

The longitudinal section of the Tunnel may be kept gradually converging& diverging or gradually converging & abruptly diverging as the endapplication needs.

The Tunnels 1, 2, 3 . . . so on & so forth may be individually shaped asa converging, or converging & diverging, or non converging nozzle tobring about required pressure &/or velocity drops to minimize the lostenergy from the outlets.

There are many different ways in which the blades can be redesigned inorder to absorb as much enthalpy as possible within the blades so theminimum is left over in the discharge. Following are few examples.

-   [A]Here the blade instead of deviating at a sharp angle bends    continuously as a smooth arc in the same plane or as a spiral arc    across different planes.-   [B]Here Tunnel-0 is tangential to the mini-axle or mega-axle. The    tip of the Tunnel takes U turn before it opens perpendicular to    broad bottom wall to be called receptor of the succeeding Tunnel, so    that the bottom wall i.e. receptor is radial to the mini-axle or    mega-axle.

There are endless numbers of end applications of SUDARSHAN CHAKRA forexample a hybrid two, three, four . . . . Wheelers used for locomotion.It can be used as a mobile battery charger on board. It can be used asself priming electric generator so on & so forth. Its use should not belimited to conversion of potential energy to kinetic energy, but canalso be used for conversion of kinetic energy to potential energy.

In the given example the tunnel is assumed to be made up of a rigidmaterial. But one can plan for a Tunnels made up of partly rigid &partly flexible material. In that case one can orient the blade eithertangential, radial or in combination of both. One drawing no 8 exhibitssuch unique blade with only one example of tunnel-0 & tunnel-1; but itcan be extrapolated further. Such arrangement would result in an actionturbine having synchronous unidirectional motion

The documents submitted here are the substitute specifications oforiginal specifications and does not contain any new matter.

1. SUDARHAN CHAKRA is a novel way invented to convert potential &/orkinetic energy from gas or liquid (propellant) into kinetic energy of arotating wheel, When the energy stored within the intermolecular motionsof gas or liquid is brought from anywhere for releasing inside cavernousmini-axle to be discharged through hollow blades yields kinetic energyin the form of revolving wheel which can have numerous furtherapplications, The invention set forth in claim 1 fulfills it byassembling a hollow mini-axle/mega-axle with numerous hollow blades, twoball bearings, two safety valves, a feeder pipe, a pulley or gear, and acylindrical Case, The invention set forth in claim 1 fulfills it with auniquely designed cavernous mini-axle having (a) An open mouth attachedto the outer diameter of mouth bearing, (b) A hollow body with numerousperforations for attaching blades, (c) A space for fixing a pulley or agear, (d) A tail having a closed or blind end attached to the innerdiameter of tail bearing, (e) Space for fixing safety valves, Theinvention set forth in claim 1 fulfills it with unique as well as noveldesign of numerous blades attached upon the perforations of the hollowaxle, These blades are not straight but bend after a regular distance ata regular angle in a uniform manner; making them bow shaped blades,having their inlets opening near the axis at the mini-axle or mega-axle;and their outlets opening just opposite to the corrugated inner liningof the Case, The sections of the blades called; Tunnel 0, 1, 2, 3, - - -; are variable in shapes, The invention set forth in claim 1 fulfills itwith two ball bearings, One near the mouth has outer diameter fixed tothe flange on inner wall of mouth of a hollow axle, another near thetail has its inner diameter fixed to the outer side of hollow mini-axlenear the tail, An imaginary line joining centers of these ball bearingsmay be called axis of the axle, The invention set forth in claim 1fulfills it with a feeder pipe whose one end is fixed to the innerdiameter of the mouth bearing and another end has a facility for leakproof attachment to the feeder supply tank, The invention set forth inclaim 1 fulfills it by fixing a pulley or a gear preferably midwaybetween mouth and tail in order to transfer torque of the mini-axle toany other machine desired to be driven by SUDARSHAN CHAKRA, Theinvention set forth in claim 1 fulfills it by fixing a cover uponaxle-blade assembly with a realistic cylindrical wall called the Casehaving a corrugated inner lining, This inner lining is planned & kept atan equal distance but slightly away from the outlets of blades, Hencethere is a clearance between the moving outlets & stationary Case, Thiscylindrical Case is oriented in such a way that its axis merges with theaxis of the axle, An adaptor may be designed for better stability & leakproof joint between moving & stationary parts.